IL207316A - Method for determining the distance of an object emitting an ir signature - Google Patents
Method for determining the distance of an object emitting an ir signatureInfo
- Publication number
- IL207316A IL207316A IL207316A IL20731610A IL207316A IL 207316 A IL207316 A IL 207316A IL 207316 A IL207316 A IL 207316A IL 20731610 A IL20731610 A IL 20731610A IL 207316 A IL207316 A IL 207316A
- Authority
- IL
- Israel
- Prior art keywords
- voltage
- detector
- wavelength
- control voltage
- wavelength filter
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S11/00—Systems for determining distance or velocity not using reflection or reradiation
- G01S11/12—Systems for determining distance or velocity not using reflection or reradiation using electromagnetic waves other than radio waves
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Investigating Or Analysing Materials By Optical Means (AREA)
- Photometry And Measurement Of Optical Pulse Characteristics (AREA)
- Length Measuring Devices By Optical Means (AREA)
- Optical Radar Systems And Details Thereof (AREA)
- Spectrometry And Color Measurement (AREA)
Description
Method for determining the distance of an object emitting an IR signature EADS Deutschland GmbH Method for determining the distance of an object emitting an IR signature The invention relates to a method for determining the distance of an object emitting an IR signature, and to an apparatus for carrying out the method.
The invention is important, in particular, when an aircraft is threatened by a self-propelled missile. Most short-range and medium-range missiles generally have an infrared homing head which is sensitive to radiation emitted by the aircraft, primarily radiation from the engines, and operates according to a target-seeking guiding method. Such guided missiles are relatively simple to produce and can also be launched from shoulder-carried weapons, so-called rocket launchers .
Since such missiles - in contrast to radar-guided missiles - passively head for their target, optical warning sensors are increasingly important in order to be able to initiate countermeasures against such approaching missiles in good time and also at the right time .
DE 195 46 873 CI proposes a method and an apparatus having a passive imaging sensor which detects the approaching object in at least two wavelength ranges in which the atmospheric attenuation coefficients are different. The object is detected in a plurality of wavelength ranges by connecting a rotating filter upstream of the optical system of the passive warning sensor, which filter consists of a plurality of sectors whose transmission ranges are different according to the selected wavelength ranges. The sensor signals corresponding to the radiation power of the approaching object at the different wavelengths, which is detected by the sensor, are now used to determine the distance and/or speed of the object, for example of a missile approaching an aircraft, taking into account the difference in the atmospheric attenuation coefficients.
The method described in DE 195 46 873 CI is based on spectrally resolved measurements at discrete wavelengths and determines the object distance by forming the ratio of two respective sensor signals in different wavelength ranges. However, this method is very inaccurate.
DE 34 14 798 Al discloses a passive rangefinder for detecting radiation from emitting objects. This rangefinder is distinguished by the fact that sun glint radiation in the wavelength range below 2.9 μπι is measured. The radiation in a so-called blue spike and a red wing is also measured. The blue spike and the red wing are respectively situated on the short-wave and long-wave sides of an atmospheric absorption band. A theoretical spectrum is generated for each wavelength in the range of wavelengths of interest from these measurements, which spectrum is weighted with a transmission factor which constitutes the proportion of radiation allowed to pass over the distance R taking into account the absorption by atmospheric carbon dioxide and nitrogen oxide. The distance to the object is determined by comparing the theoretical and experimental results.
The object of the invention is to specify a method and an apparatus which can be used to provide data relating to an approaching object in a faster and more accurate manner than in the prior art.
This object is achieved, with regard to the method, with the subject matter of patent claim 1 and, with regard to the apparatus, with the subject matter of patent claim 11. Subclaims respectively relate to advantageous embodiments of the invention.
According to the method, the spectral intensity distribution (also referred to as the intensity distribution spectrum) of a detected object is measured in the region of an absorption structure of the atmosphere. A point having an extremal gradient on a flank of an intensity rise or fall, caused by the atmospheric absorption structure, in the measured intensity distribution spectrum is determined in the measured intensity distribution spectrum. The path length which is traveled by the radiation through the atmosphere and corresponds to the distance between the detector and the object is determined by comparison with known transmission data for the atmosphere. The temporal shift in the position is also expediently determined from corresponding distance measurements at two different points in time and is used to calculate the relative speed between the detector and the object. In this case, the intensity distribution spectrum can be recorded with regard to the wavelength or the frequency .
In other words, the method according to the invention makes it possible to determine the spectral position of the flank of the spectral intensity distribution at different points in time using the point having a maximum gradient. This is considerably more accurate than the determination, as described in DE 195 46 873 CI, by forming the ratio of discrete measurements at different wavelengths and is largely independent of the spectral distribution of the intensity emitted by the object, since only a narrow wavelength range has to be evaluated.
The spectral intensity distribution is expediently investigated in a wavelength range which is. in the region of atmospheric absorption lines, preferably in the vicinity of those absorption lines which are caused by gases whose concentration fluctuates only slightly with the climatic conditions. The wavelength range of, for example, 4-5 μπι, expediently of 4.3-4.7 μχα, which is in the mid-infrared on the short-wave and long-wave sides of the C02 absorption line is particularly suitable for this purpose. It goes without saying that the spectral intensity distribution can also be investigated in a corresponding frequency range.
The apparatus according to the invention comprises input optics with an electrically tunable wavelength filter having a voltage-dependent filter characteristic curve, a passively imaging detector for detecting the radiation from the object, a first circuit for processing the detector signal, and a second circuit for generating a periodically varying control voltage for the wavelength filter. The first circuit is expediently constructed from a differentiating element, an analog/digital converter and a signal analysis processor, and the second circuit is essentially constructed from a function generator, a clock generator and a summation element. The apparatus also comprises a voltage source for generating an offset voltage for the voltage to be supplied to the wavelength filter.
The method according to the invention makes it possible to completely detect and evaluate the entire IR radiation emitted by an object at any point in time. The entire two-dimensional image field of an object to be investigated is thus detected. The apparatus according to the invention is thus used to supply all radiation focused by the lens into the image plane to spectral evaluation. In contrast to the prior art, as described in GB 2 323 730 A for example, the entire object rather than object sections is considered in principle .
The invention and advantageous refinements are explained in more detail below using drawings, in which : fig. 1 shows the schematic structure of an apparatus according to the invention, fig. 2 shows the atmospheric CO2 absorption as a function of the distance between the detector and the object and the wavelength, fig. 3 shows the profile of the detector signal and of the control signal as a function of time.
Fig. 1 illustrates the schematic structure of an apparatus according to the invention. The apparatus according to the invention is essentially a sensor having input optics 1, in the form of a lens, and an electrically tunable wavelength filter 2 which is arranged upstream of a detector 3. The wavelength filter 2 may be, for example, a silicon-based Fabry-Perot filter.
The detector signals are supplied to a signal analysis processor 6 via a differentiating . element 4 and an analog/digital converter 5. The signal analysis processor 6 controls, on the one hand, a clock generator 9 for generating a temporal reference signal. On the other hand, the signal analysis processor 6 controls a voltage source 10. The clock generator 9 supplies the temporal reference signal to a function generator 8 for generating a periodically varying voltage. This periodic voltage and the voltage from the voltage source are added in a summation element 7 and are supplied to the wavelength filter 2 as a control voltage. This control voltage thus has a constant voltage component, resulting from the voltage source 10, and a periodic voltage component, resulting from the function generator 8.
According to the invention, the electrically tunable wavelength filter is driven in such a manner that a wavelength range Δλ around a fixed, center wavelength λ0 is periodically scanned according to the relationship A(t) = λ0 + Δλ · P(t) (1) where P(t) denotes a temporally periodic function.
In order to control the electrically tunable wavelength filter, a periodically varying voltage (for example sinusoidal, triangular-waveform or saw-tooth) is correspondingly generated at an offset. For a control voltage of U (t) = Uo + AU · cos (cot) , the following is obtained with the aid of the characteristic curve f(U) of the wavelength filter A(t) = f(U0) + f(AU · cos(wt)) (2).
In this case, the offset voltage U0 stipulates the center wavelength λ0, and the amplitude AU determines the scanning wavelength range Δλ.
The parameters U0 and AU are selected in such a manner that the spectral features of the object signature which are to be detected are in the scanning range. The detector signal generated in this manner is differentiated and is converted into digital signals which are processed by a signal analysis processor which extracts the spectral features. As a result of differentiation, the proportion of spectrally unstructured background radiation in the signal is omitted, and the spectral features of the object radiation are highlighted more clearly.
The processor assigns the extracted spectral features to the wavelength by temporally referencing the digitized detector signal to the clock; signals from the clock generator and thus to the control voltage instantaneously applied to the wavelength filter.
If the distance determination with the aid of the spectral flank produced by the atmospheric COz absorption at wavelengths of between 4 μπι and 5 μπι is specifically considered, the parameters for scanning the wavelength' range can be advantageously selected as λ0 = 4.5 pm and Δλ = 0.15 im according to the bottom of fig. 2. The upper part of fig. 2 shows the atmospheric transmission as a function of the wavelength for the distances of 500 m, 1000 m, 2000 m and 4000 m between the object and the detector. The lower part illustrates the respective differential.
These parameters give a periodically varying detector signal which is shown in fig. 3 together with the control voltage for the wavelength filter according to equation (2). Relative units are plotted against the argument of the cos function of the control voltage, expressed as an angle in degrees. A check is first of all carried out in order to determine whether the magnitudes of the maximum and minimum in the differentiated detector signal exceed a predetermined threshold value. If this is the case, there is a significant intensity flank in the detected range of the detector signal. The time of the zero crossing in the periodic component of the control voltage is then selected as a reference to, and the offset Δ, as the difference from the position of the maximum in the differentiated detector signal, is obtained as the measurement variable which is determined by the processor .
Methods for extracting a peak position from an electrical signal are known, for example, from US 4 658 368. The offset Δ and thus also the temporal shift At between the peak position and the zero crossing in the periodic component of the control voltage can thus be determined, from which the associated wavelength A(to+At) is then also obtained using the associated value of the control voltage U(t0+At) and the characteristic curve of the wavelength filter. The sought position of the spectral flank is thus determined .
In a first particular embodiment of the invention, a closed control loop can be produced by using the offset Δ as a controlled variable for tracking the magnitude of the reference voltage in such a manner that the offset Δ is adjusted to zero. The positions of the extremes in the differentiated detector signal thus coincide with the zero crossings of the reference signal. The control loop is illustrated in fig. 1 by means of the dashed connection between the processor and the reference voltage source. In this case, the sought position of the spectral flank is obtained from the conversion of the magnitude of the regulated reference voltage using the characteristic curve of the wavelength filter.
In a second particular embodiment of the invention for determining the controlled variable Δ for tracking the reference voltage, the approximately fulfilled symmetry of the differentiated detector signal in the vicinity of the maximum is used. An interval of time of a suitable magnitude is accordingly selected symmetrically around the time to of the zero crossing in the periodic component of the control voltage. Within this interval, each digitized value of the differentiated detector signal is multiplied by the associated value of the periodic component of the reference signal and all products obtained in this manner are added. Since the periodic component of the reference signal is an odd function with respect to to, the result becomes zero if the controlled variable Δ disappears. The sum of the products is thus suitable as the controlled variable.
The invention makes it possible to reference to characteristic features of the spectral intensity distribution in a more accurate manner. For instance, the spectral position of a flank caused by atmospheric absorption can be determined exactly and can be tracked over time by driving the wavelength filter with a periodically varying voltage at an offset and evaluating the detector signal with the aid of (analog or digital) differentiation and peak detection. Peak detection can then be used to derive a control signal for tracking the offset voltage of the wavelength filter, with the result that this voltage always tunes the filter to the position of the flank of the spectral intensity distribution.
This results in the advantage that the spectral position of the flank is determined using the point having a maximum gradient; this is considerably more accurate than the determination by forming the ratio of discrete measurements at different wavelengths and is largely independent of the spectral distribution of the intensity emitted by the object. Tracking the offset voltage means that the spectral flank is always spectrally resolved in an optimal manner irrespective of its respective spectral position. Further advantages result from the type of processing of the detector signal, which improves the signal-to-noise ratio and is suitable, in particular, for detecting weak structures on a high base (differentiation) .
Claims (12)
1. A method for determining the distance of an object emitting an IR signature, the spectral intensity distribution of the radiation emitted by the object in a predefined wavelength range being detected, characterized in that an intensity distribution spectrum of the object is measured in the region of an absorption structure of the atmosphere, a point having an extremal gradient on a flank of an intensity rise or fall, caused by the atmospheric absorption structure, is determined in the measured intensity distribution spectrum, and the path length traveled by the radiation through the atmosphere and therefore also the distance between the detector and the object are determined by comparison with known transmission data for the atmosphere.
2. The method as claimed in claim 1, characterized in that the distance between the detector and the object is determined at two different points in time, and the relative speed between the detector and the object is calculated from the temporal shift in the position.
3. The method as claimed in claim 1 or 2, characterized in that the spectral intensity distribution is detected using a detector and an electrically tunable wavelength filter, and a control voltage is supplied to the wavelength filter for the purpose of controlling the filter properties.
4. The method as claimed in claim 3, characterized in that the control voltage has a periodically varying voltage component Δϋ" and a predefinable fixed offset voltage component U0.
5. The method as claimed in claim 3 or 4, characterized in that the detector signal is differentiated in a first step, is digitized in a second step and, in a third step, is referenced to the control voltage instantaneously applied to the wavelength filter.
6. The method as claimed in claim 5, characterized in that maxima and minima in the differentiated detector signal are compared with predefinable threshold values, and, if the magnitudes of the extremes exceed the threshold value, an offset Δ in the form of a temporal shift At is determined as the difference between the maximum in the differentiated detector signal and the time tO of the zero crossing in the periodic component of the control voltage, from which the associated wavelength X(t0+At) is determined using the associated value of the control voltage U(t0+At) and the characteristic curve of the wavelength filter.
7. The method as claimed in claim 6, characterized in that a variable which is proportional to the offset Δ is used as a controlled variable for tracking the magnitude of the control voltage, the offset Δ being regulated to zero.
8. The method as claimed in claim 6, characterized in that an interval of time is selected symmetrically around the time tO, and in that the sum of the products of each digitized value of the differentiated detector signal with the associated value of the periodic component of the control signal is calculated within the interval of time.
9. The method as claimed in one of the preceding claims , characterized in that the wavelength range is in the vicinity of atmospheric absorption lines, preferably in the vicinity of those absorption lines which are caused by gases whose concentration fluctuates only slightly with the climatic conditions.
10. The method as claimed in claim 9, characterized in that the wavelength range in the mid-infrared on the short-wave and long-wave sides of the C02 absorption line is at approximately 4.25 μπι.
11. An apparatus for carrying out a method as claimed in one of the preceding claims, having input optics with an electrically tunable wavelength filter having a voltage-dependent filter characteristic curve, a passively imaging detector for detecting the entire two-dimensional image field of an object to be investigated, a first circuit for processing the detector signal, and a second circuit for generating a periodically varying control voltage for the wavelength filter , the first circuit comprises a differentiating element, an analog/digital converter and a signal analysis processor.
12. The apparatus as claimed in claim 11, characterized in that the second circuit comprises a function generator for generating a periodically varying voltage, a clock generator and a summation element for summing the periodically varying voltage generated by the function generator with the voltage from a constant voltage source. The apparatus as claimed in claim 12, characterized in that the first circuit and the second circuit form a closed control loop together with the constant voltage source. the Applicant
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008011123A DE102008011123B4 (en) | 2008-02-26 | 2008-02-26 | Method for determining the distance of an object emitting an IR signature |
PCT/DE2009/000186 WO2009106037A1 (en) | 2008-02-26 | 2009-02-10 | Method for determining the distance of an object emitting an ir signature |
Publications (2)
Publication Number | Publication Date |
---|---|
IL207316A0 IL207316A0 (en) | 2010-12-30 |
IL207316A true IL207316A (en) | 2014-06-30 |
Family
ID=40791626
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL207316A IL207316A (en) | 2008-02-26 | 2010-07-29 | Method for determining the distance of an object emitting an ir signature |
Country Status (7)
Country | Link |
---|---|
US (1) | US8586929B2 (en) |
EP (1) | EP2250516B1 (en) |
DE (1) | DE102008011123B4 (en) |
ES (1) | ES2606252T3 (en) |
IL (1) | IL207316A (en) |
WO (1) | WO2009106037A1 (en) |
ZA (1) | ZA201005253B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2962827B1 (en) * | 2010-07-13 | 2013-05-10 | Thales Sa | METHOD AND DEVICE FOR BI-SPECTRAL MULTIFUNCTION IMAGING |
JP5919728B2 (en) * | 2011-10-26 | 2016-05-18 | セイコーエプソン株式会社 | Spectrometer |
JP2013181912A (en) * | 2012-03-02 | 2013-09-12 | Seiko Epson Corp | Component analyzer |
DE102012007677B4 (en) * | 2012-04-17 | 2015-05-07 | Airbus Defence and Space GmbH | Optical sensor arrangement |
JP6146100B2 (en) * | 2012-06-21 | 2017-06-14 | Jsr株式会社 | Liquid crystal aligning agent, liquid crystal aligning film, retardation film, liquid crystal display element and method for producing retardation film |
JP6098051B2 (en) * | 2012-07-04 | 2017-03-22 | セイコーエプソン株式会社 | Spectrometer |
DE102016013960A1 (en) | 2016-11-23 | 2018-05-24 | Hensoldt Sensors Gmbh | Infrared optical missile warning system and method of using such a system |
WO2019034836A1 (en) * | 2017-08-14 | 2019-02-21 | Bae Systems Plc | Passive sense and avoid system |
EP3447527A1 (en) * | 2017-08-21 | 2019-02-27 | BAE SYSTEMS plc | Passive sense and avoid system |
Family Cites Families (15)
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US3026413A (en) * | 1952-11-01 | 1962-03-20 | Rca Corp | Determining the range of an infra-red source with respect to a point |
GB2323730B (en) * | 1983-04-21 | 1999-01-13 | Secr Defence | Passive identification and rangefinder apparatus |
US4658368A (en) | 1985-04-30 | 1987-04-14 | Canadian Patents And Development Limited-Societe Canadienne Des Brevets Et D'exploitation Limitee | Peak position detector |
US4883963A (en) * | 1986-04-28 | 1989-11-28 | Bran+Luebbe Gmbh | Optical analysis method and apparatus having programmable rapid random wavelength access |
GB8710567D0 (en) * | 1987-05-05 | 1998-07-08 | Secr Defence | A passive rangefinder |
US5282013A (en) * | 1992-06-26 | 1994-01-25 | Spar Aerospace Limited | Passive ranging technique for infrared search and track (IRST) systems |
US5469265A (en) * | 1992-12-02 | 1995-11-21 | Measures; Raymond M. | Method and apparatus for an optoelectronic smart structure interface with wavelength demodulation of laser sensors |
US5489265A (en) * | 1994-06-15 | 1996-02-06 | Ivac Corporation | Restrictor fitting for an infusion pump |
DE69532191T2 (en) * | 1994-09-20 | 2004-09-09 | Noritsu Koki Co., Ltd. | METHOD AND DEVICE FOR TRANSPORTING PHOTO SENSITIVE MATERIALS |
US5677761A (en) * | 1995-07-25 | 1997-10-14 | Textron Systems Corporation | Passive ranging to source of known spectral emission |
US6222618B1 (en) * | 1995-07-25 | 2001-04-24 | Textron Systems Corporation | Passive ranging to source of known spectral emission |
FR2738630B1 (en) | 1995-09-08 | 1997-10-24 | Thomson Csf | METHOD FOR CLASSIFYING THREATS BY BISPECTRAL INFRARED DETECTION AND CORRESPONDING WATCH DEVICE |
DE19546873C1 (en) | 1995-12-15 | 1997-05-15 | Daimler Benz Aerospace Ag | Determining distance of object flying through atmosphere and radiating energy |
DE19646873C2 (en) | 1996-11-13 | 2000-06-21 | Joerg Schrickel | Progressive torsion bar suspension with integrated damping unit for vehicles |
US6894343B2 (en) * | 2001-05-18 | 2005-05-17 | Sandisk Corporation | Floating gate memory cells utilizing substrate trenches to scale down their size |
-
2008
- 2008-02-26 DE DE102008011123A patent/DE102008011123B4/en not_active Expired - Fee Related
-
2009
- 2009-02-10 ES ES09714658.3T patent/ES2606252T3/en active Active
- 2009-02-10 US US12/919,669 patent/US8586929B2/en not_active Expired - Fee Related
- 2009-02-10 EP EP09714658.3A patent/EP2250516B1/en active Active
- 2009-02-10 WO PCT/DE2009/000186 patent/WO2009106037A1/en active Application Filing
-
2010
- 2010-07-23 ZA ZA2010/05253A patent/ZA201005253B/en unknown
- 2010-07-29 IL IL207316A patent/IL207316A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
DE102008011123A1 (en) | 2009-09-10 |
WO2009106037A1 (en) | 2009-09-03 |
US8586929B2 (en) | 2013-11-19 |
ZA201005253B (en) | 2011-03-30 |
IL207316A0 (en) | 2010-12-30 |
DE102008011123B4 (en) | 2012-09-06 |
EP2250516B1 (en) | 2016-09-14 |
ES2606252T3 (en) | 2017-03-23 |
EP2250516A1 (en) | 2010-11-17 |
US20110058152A1 (en) | 2011-03-10 |
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